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LDSD POST2 Modeling Enhancements in Support of SFDT-2 Flight OperationsProgram to Optimize Simulated Trajectories II (POST2) was utilized to develop trajectory simulations characterizing all flight phases from drop to splashdown for the Low-Density Supersonic Decelerator (LDSD) project's first and second Supersonic Flight Dynamics Tests (SFDT-1 and SFDT-2) which took place June 28, 2014 and June 8, 2015, respectively. This paper describes the modeling improvements incorporated into the LDSD POST2 simulations since SFDT-1 and presents how these modeling updates affected the predicted SFDT-2 performance and sensitivity to the mission design. The POST2 simulation flight dynamics support during the SFDT-2 launch, operations, and recovery is also provided.
Document ID
20160007701
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
White, Joseph
(Analytical Mechanics Associates, Inc. Hampton, VA, United States)
Bowes, Angela L.
(NASA Langley Research Center Hampton, VA, United States)
Dutta, Soumyo
(NASA Langley Research Center Hampton, VA, United States)
Ivanov, Mark C.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Queen, Eric M.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
June 20, 2016
Publication Date
February 14, 2016
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NF1676L-22644
AAS Paper 16-221
Meeting Information
Meeting: AAS/AIAA Space Flight Mechanics Meeting
Location: Napa, CA
Country: United States
Start Date: February 14, 2016
End Date: February 18, 2016
Sponsors: American Astronautical Society, American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 406979.01.07.06
Distribution Limits
Public
Copyright
Public Use Permitted.
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